Tecnam P2006T, Aircraft Flight Manual

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Page G7-8
Section 9 – Supplements
Supplement no. G7 – AFM Supplement for CIS countries operators
3
rd
Edition, Rev. 0
EMERGENCY PROCEDURES
S
MOKE AND FIRE OCCURRENCE
Use ventilation window in case of smoke in cabin for all cases.
F
AILURE OF
C
ONTROL
S
YSTEM
L
OSS OF
S
TABILATOR
C
ONTROL
In case of loss of pilot side stabilator control (disconnected or jammed), apply following pro-
cedure:
1. Continue the flight at the speed of 80 - 85 KIAS due to the aircraft weight in cruise
configuration.
2. Bank angle: not more than 30° during turning.
3. Control the aircraft with mechanical trim and engine power setting.
The increase of thrust causes a nose up moment; the decrease of thrust
causes a nose down moment. The control by trim operation is related to
the trim position: trim UP for aircraft nose Up; trim DOWN for aircraft
nose DOWN.
CAUTION
Perform approach and landing only in cruise configuration (Flap 0°).
It is necessary to move the landing gear in down position before starting
the glide and to balance the aircraft with trim and thrust.
It is possible to correct the glide path by trim operation to minimize the
thrust engines changes.
Only after touchdown it is possible to move the engine controls in idle
position.
Land as soon as possible.
NOTE